基于DXF的OpenFlight数据创建方法研究

针对虚拟城市仿真系统应用中OpenFlight模型缺乏、建模方式单一,难以构建复杂模型的情况,本文提出基于CAD文件来构建Opeflght模型的方法,在详细分析OpenFlight和DXF的数据组织结构的基础上,设计了基于DXF的OpenFlight数据创建方案并编程实现。通过实例测试证明该方案能快速、完整地进行数据转换,为虚拟城市系统的三维仿真模型构建提供了一条行之有效的途径。     

砂芯的第四纪环境遗迹研究值得重视——第四纪孢粉环境信息对全球环境研究的倡议

1996年春,天津地质调查中心海岸带与第四纪地质研究所参加了新疆地矿局在塔克拉玛干沙漠的地下水勘查工作,负责沙漠中心区KT1孔(塔中南侧38km处,38°47′N,83°57′E,孔深653.8m)的野外岩芯编录、取样和综合研究。KT1孔基本上是砂层与泥质沉积的互层,大致划分为212层、106个互层、53个中     

Strain-softening behaviour of sand in strain path testing under plane-strain conditions

Experimental data are presented in this paper to study the strain-softening behaviour of sand under plane-strain conditions. K ₀ consolidated strain path tests were conducted using a new plane-strain apparatus. The stress–strain behaviour of medium dense sand under plane-strain conditions was characterized. The test results show that the occurrence of pre-failure strain softening under plane-strain conditions is affected by the void ratio, the strain increment ratio and the initial effective confining stress. This is consistent with previous findings established under axisymmetric conditions. However, a pre-failure strain-softening behaviour in plane-strain tests conducted under high-confining stresses may consist of three stages, namely, material softening, banding softening, and ultimate state. This observation is different from that in triaxial tests where banding softening does not normally occur.     

SOMATOM AR.C型CT机复位故障检修

本文介绍了由电源故障引起的不可逆转故障,并讨论了维修和故障的排除。     

Strain softening of K0-consolidated Changi sand under plane-strain conditions

Experimental results are presented in this paper to study the strain softening behaviour of a marine dredged sand under plane-strain conditions. K₀ consolidated drained and undrained tests were conducted using a new plane-strain apparatus to characterize the strain softening behaviour of the sand under plane-strain conditions. For medium dense specimens, strain softening and shear bands were observed to occur under both drained and undrained conditions. For very loose specimens, no shear bands were observed and critical states were reached within the homogeneous deformation region in both drained and undrained tests. Strain softening was observed to occur at small strain for very loose specimens under undrained conditions. Two types of strain softening, the homogenous softening and banding softening, were identified and the conditions for strain softening were established. The results obtained from this study were compared with the studies by Han and Vardoulakis (Géotechnique 41(1):49–78, 1991), Finno et al. (J Geotech Eng ASCE 122(6):462–473, 1996, Géotechnique 47(1):149–165, 1997) and Mokni and Desrues (Mech Cohes-Frict Mat 4:419–441, 1998).     

Relationship of Uncertainty and Line Segment for Between Polygon Segment Spatial Data in GIS

The mathematic theory for uncertainty model of line segment are summed up to achieve a general conception, and the line error hand model of εσ is a basic uncertainty model that can depict the line accuracy and quality efficiently while the model of εm and error entropy can be regarded as the supplement of it. The error band model will reflect and describe the influence of line uncertainty on polygon uncertainty. Therefore, the statistical characteristic of the line error is studied deeply by analyzing the probability that the line error falls into a certain range. Moreover, the theory accordance is achieved in the selecting the error buffer for line feature and the error indicator. The relationship of the accuracy of area for a polygon with the error loop for a polygon boundary is deduced and computed.     

车载智能地理信息查询系统及其自然语言接口

车载地理查询系统涉及到多方面的软、硬件技术和数据来源；本文提出了车载系统所需具备的主要功能，并对其中所需解决的关键问题进行了讨论。特别是针对如何使车载系统具备一定的智能问题，提出了将自然语言和空间查询语句结合，构造模式库，在自然语言识别处理的基础上，完成自然语言空间查询的方法。     

FORMOSAT-3/COSMIC science mission update

The FORMOSAT-3/COSMIC mission is a microsatellite mission for weather forecast, climate monitoring, and atmospheric, ionospheric and geodesy research. This mission is a collaborative Taiwan-USA science experiment to deploy a constellation of six microsatellites in low Earth orbits. The mission life is 2 years with a goal of 5 years. The final mission orbit has an altitude of 750–800 km. Each satellite consists of three science payloads: global positioning system (GPS) occultation experiment (GOX) payload, tiny ionospheric photometer (TIP) and tri-band beacon (TBB). The GOX will collect the GPS signals for the study on atmosphere, ionosphere, and geodesy. The TIP and TBB can provide the electron distribution information for ionospheric research. The deployment of the FORMOSAT-3 constellation and the resulting influence on the occultation sounding distributions are reported. Details are also given on GOX, TIP, and TBB payload operations and the contributions of the Taiwan Science Team.